US6435825B1 - Hollow nozzle partition with optimized wall thickness and method of forming - Google Patents
Hollow nozzle partition with optimized wall thickness and method of forming Download PDFInfo
- Publication number
- US6435825B1 US6435825B1 US09/681,452 US68145201A US6435825B1 US 6435825 B1 US6435825 B1 US 6435825B1 US 68145201 A US68145201 A US 68145201A US 6435825 B1 US6435825 B1 US 6435825B1
- Authority
- US
- United States
- Prior art keywords
- partition
- partitions
- hollow nozzle
- interior plate
- forming
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/70—Treatment or modification of materials
- F05D2300/702—Reinforcement
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
Definitions
- the invention relates to a hollow nozzle partition used in, for example, a boiling water reactor (BWR) environment, and, more particularly to a hollow nozzle partition with plates welded onto inner sidewalls of the partition to prevent wall buckling or ballooning under certain operating conditions.
- BWR boiling water reactor
- Hollow nozzle partition designs are used in fossil-fueled steam generating plants and reach lengths of at least 33.5′′.
- a hollow nozzle partition is formed from two curved metal plates, a convex plate 10 and concave plate 12 , joined along their seams 14 , 16 , typically, by welding.
- End cap 11 may be welded at one (or both open ends) to form an enclosed hollow nozzle partition. Only one end cap 11 is needed where the other open end is closed off by attachment of the hollow nozzle partition to a turbine ring or the like.
- Pressurized water reactor (PWR) nuclear power plants also currently use hollow nozzle partitions.
- the hollow nozzle partitions provide substantial cost savings versus solid partitions in nuclear, low-pressure, environments where partition lengths reach roughly between 38′′ and 52′′.
- Nuclear units are intrinsically wet environments where relative humidity can reach 11% or higher at the last stage diaphragm in the low-pressure section. A result of this moisture running through the unit is increased erosion of the steel components, thus causing small particulates to travel along the steam path.
- BWR boiling water reactor
- water passes and comes in contact with the reactor core this is opposed to a PWR unit where the water is contained within piping and does not come into contact with the core. Any suspended solids due to erosion will become irradiated by the reactor core and will thus be carried by the steam throughout the turbine.
- the above described problems in the prior art hollow nozzle partitions are solved by the present invention which incorporates at least one welded plate onto at least one of the hollow partition inner sidewalls.
- the welded plates prevent wall buckling and ballooning failure modes by optimizing the wall thickness and strength to withstand any sudden increase in internal pressure caused by steam flash due to entrapped moisture.
- the welded plate need not extend completely from one inner side wall to the opposite facing inner side wall, nor need it extend along the entire length of the partition.
- the ability of the hollow nozzle partition to withstand wall buckling and ballooning can be achieved by a plate that only extends partly into the interior of the hollow nozzle partition and only partly along the length of the hollow nozzle partition. Multiple plates can be welded onto one or more inner surfaces of the hollow nozzle partition.
- the invention provides the advantages of reduced cost, weight, and machining complexity as compared to conventional nozzle partition designs. Theses advantages result from the use of lighter grade steel for the hollow nozzle partition plates, since increased strength can be realized by employing the interior plates.
- FIG. 1 is a conventional prior art hollow partition with vent holes
- FIG. 2 is a perspective view of a first exemplary embodiment of the present invention.
- FIG. 3 is a perspective view of a second exemplary embodiment of the present invention.
- FIG. 4 is a perspective view of a third exemplary embodiment of the present invention.
- the invention comprises convex half partition 10 and concave half partition 12 which are formed out of sheet metal and then welded along seams 14 , 16 , and machined to the final shape. At least one plate 20 is then welded onto an inner surface of convex half partition 10 .
- a stiffening effect takes place thus increasing the critical buckling and yielding stresses of the sidewalls.
- plate 20 could be welded onto the inner surface of convex half partition 10 before welding it to concave half partition 12 , with the same stiffening effect resulting. End caps have not been shown in any of FIGS. 2-4 so that the details of the interior plates can be shown.
- At least one plate 22 is welded onto an inner surface of concave half partition 12 .
- plate 22 can be welded onto an inner surface of concave half partition 12 before or after it is assembled with convex half partition 10 .
- one or more plates 24 are welded to both half partitions 10 and 12 . Plates 24 provide even greater stiffening effect by extending from one side to the other of the hollow nozzle partition.
- Another instance of this invention would be to weld one or more plates to either adjacent inner wall surface from the open partition end once the partition has been assembled. Accordingly, the aspect ratio of the sidewall is reduced and, thus, the susceptibility to ballooning is reduced. This arrangement also increases the overall stiffness of the partition.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Butt Welding And Welding Of Specific Article (AREA)
Abstract
Description
Claims (8)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/681,452 US6435825B1 (en) | 2001-04-10 | 2001-04-10 | Hollow nozzle partition with optimized wall thickness and method of forming |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/681,452 US6435825B1 (en) | 2001-04-10 | 2001-04-10 | Hollow nozzle partition with optimized wall thickness and method of forming |
Publications (1)
Publication Number | Publication Date |
---|---|
US6435825B1 true US6435825B1 (en) | 2002-08-20 |
Family
ID=24735337
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/681,452 Expired - Fee Related US6435825B1 (en) | 2001-04-10 | 2001-04-10 | Hollow nozzle partition with optimized wall thickness and method of forming |
Country Status (1)
Country | Link |
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US (1) | US6435825B1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070166151A1 (en) * | 2006-01-13 | 2007-07-19 | General Electric Company | Welded nozzle assembly for a steam turbine and methods of assembly |
US20070292266A1 (en) * | 2006-01-13 | 2007-12-20 | General Electric Company | Welded nozzle assembly for a steam turbine and related assembly fixtures |
US20110211946A1 (en) * | 2006-01-13 | 2011-09-01 | General Electric Company | Welded nozzle assembly for a steam turbine and assembly fixtures |
US20140255207A1 (en) * | 2012-12-21 | 2014-09-11 | General Electric Company | Turbine rotor blades having mid-span shrouds |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1706703A (en) * | 1923-04-20 | 1929-03-26 | Thomas E Murray | Method of production of turbine blandes |
US3627443A (en) * | 1968-09-04 | 1971-12-14 | Daimler Benz Ag | Turbine blade |
US3729930A (en) * | 1970-06-23 | 1973-05-01 | Rolls Royce | Gas turbine engine |
US4507051A (en) * | 1981-11-10 | 1985-03-26 | S.N.E.C.M.A. | Gas turbine blade with chamber for circulation of cooling fluid and process for its manufacture |
-
2001
- 2001-04-10 US US09/681,452 patent/US6435825B1/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1706703A (en) * | 1923-04-20 | 1929-03-26 | Thomas E Murray | Method of production of turbine blandes |
US3627443A (en) * | 1968-09-04 | 1971-12-14 | Daimler Benz Ag | Turbine blade |
US3729930A (en) * | 1970-06-23 | 1973-05-01 | Rolls Royce | Gas turbine engine |
US4507051A (en) * | 1981-11-10 | 1985-03-26 | S.N.E.C.M.A. | Gas turbine blade with chamber for circulation of cooling fluid and process for its manufacture |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070166151A1 (en) * | 2006-01-13 | 2007-07-19 | General Electric Company | Welded nozzle assembly for a steam turbine and methods of assembly |
US20070292266A1 (en) * | 2006-01-13 | 2007-12-20 | General Electric Company | Welded nozzle assembly for a steam turbine and related assembly fixtures |
US7427187B2 (en) | 2006-01-13 | 2008-09-23 | General Electric Company | Welded nozzle assembly for a steam turbine and methods of assembly |
US7997860B2 (en) | 2006-01-13 | 2011-08-16 | General Electric Company | Welded nozzle assembly for a steam turbine and related assembly fixtures |
US20110211946A1 (en) * | 2006-01-13 | 2011-09-01 | General Electric Company | Welded nozzle assembly for a steam turbine and assembly fixtures |
US8702385B2 (en) | 2006-01-13 | 2014-04-22 | General Electric Company | Welded nozzle assembly for a steam turbine and assembly fixtures |
US20140255207A1 (en) * | 2012-12-21 | 2014-09-11 | General Electric Company | Turbine rotor blades having mid-span shrouds |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: GENERAL ELECTRIC COMPANY, NEW YORK Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:KIRBY, GEORGE HORNER, III;FLORIN, MARK ARNE;REEL/FRAME:011931/0897;SIGNING DATES FROM 20010524 TO 20010618 |
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FPAY | Fee payment |
Year of fee payment: 4 |
|
FPAY | Fee payment |
Year of fee payment: 8 |
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SULP | Surcharge for late payment |
Year of fee payment: 7 |
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FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
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REMI | Maintenance fee reminder mailed | ||
LAPS | Lapse for failure to pay maintenance fees | ||
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
|
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20140820 |